As a first attempt, the dynamic responses of sandwich truncated conical shells with graphene platelets
reinforced composite (GPLRC) face sheets, porous core and circumferential stiffeners under asymmetric internal
ring-shaped moving load are analyzed. The face sheets and porous core are reinforced by uniformly distributed
and randomly oriented graphene platelets (GPLs). The spatially discretized equations of motion subjected to
different boundary conditions are derived based on the first-order shear deformation theory (FSDT) using the
Chebyshev–Ritz method. The admissible functions of the field variables are constructed using the trigonometric
functions in the circumferential direction and the one-dimensional Chebyshev polynomials in conjunction
with the suitable boundary functions in the meridional direction. The Newmark’s time integration scheme
is employed to solve the resulting ordinary differential equations of motion. The robustness and accuracy of
the method are demonstrated through the different examples. After that, the influences of core porosity, face
sheets, GPLs parameters, shell geometric parameters, boundary conditions, and the arrangement, number and
size of stiffeners on the results are explored. The results show that porosity, face sheets, the location, size and
number of stiffeners play important roles on the dynamical response of the shells under investigation. Also,
it is found that the critical load velocity decreases by increasing the porosity coefficients and increases by
increasing the number of ring-stiffeners.